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Synchronously deployable truss structureA collapsible-expandable truss structure, including first and second spaced surface truss layers having an attached core layer is described. The surface truss layers are composed of a plurality of linear struts arranged in multiple triangular configurations. Each linear strut is hinged at the center and hinge connected at each end to a nodular joint. A passive spring serves as the expansion force to move the folded struts from a stowed collapsed position to a deployed operative final truss configuration. A damper controls the rate of spring expansion for the synchronized deployment of the truss as the folded configuration is released for deployment by the restrain belts. The truss is synchronously extended under the control of motor driven spools.
Document ID
19860016317
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Bush, H. G.
(NASA Langley Research Center Hampton, VA, United States)
Mikulas, M., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Wallsom, E.
(Kentron International, Inc. Hampton, Va., United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1986
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Number: US-PATENT-4,578,920
Patent Application Number: US-PATENT-APPL-SN-556512
Patent Number: NASA-CASE-LAR-13117-1
Accession Number
86N25789
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,578,920|NASA-CASE-LAR-13117-1
Patent Application
US-PATENT-APPL-SN-556512
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